ATAR 101 E5

air turbine starter

Coleoptère

Coleoptère

Nord Griffon II

Nord Griffon II

1952 SNCASO S.O. 4050-03 Vautour

Dassault Etendard

ATAR 101 G3

1956 Dassault Mirage III-001

Dassault Super Mystère B2

1956 Dassault Super Mystère B2

B1 B2 C D E 08C 1957(+reheat) F G

-9 stage compressor (airflow +15%)-last 3 stages in steel-2-stage turbine-systems below engine-eyelid exhaust nozzles

produced: 176

ATAR 101 E5 8C

year 1956 1957

thrust (lbf) 8160 9700

rpm 8400 8400

TET (C°) 865 885(F°) 1590 1625

pressure ratio: 4.8 5.8

compressor stages: 8 9max. diameter (mm/in):920 / 36.2

1956 Dassault Étendard IV M

ATAR 101 08C

B1 B2 C D E 08C(+reheat) F G 09B 1957

-all compressor stages in steel

lowest specific mass in the world:0.227 lb/lbf - thrust/weight ratio: 4.4

produced: 419

ATAR 101 8C 9B

year 1957 1957

thrust (lbf) 9700 9400(reheat) (13 200)

rpm 8400 8400

TET (C°) 885 885(F°) 1625 1625

pressure ratio: 5.8 5.7

compressor stages: 9 9max. diameter (mm/in):920 / 36.2 1020 / 40.2

ATAR 101 09B

Dassault Mirage IIIC

SEPR 844

SEPR 844

Dassault Mirage IIIO

B1 B2 C D E 8C(+reheat) F G 9B 9C 1960

-multiflap exhaust nozzle-starter: Microturbo Noelle 60

produced: 1671

Microturbo NOELLE 60290

diameter: 312 mmlength: 613 mm

Electric starter:27000 rpm

Turbine engine:47000 rpmFree turbine

Mirage IIICJ

IAI Kfir

Mirage 5

9K50

9K

9C

B1 B2 C D E 8C(+reheat) F G 9B 9C 9K 1961

-first 2 stages transsonic-electronic TET/rpm management

produced: 248

ATAR 101 9B 9K

year 1957 1961

thrust (lbf) 9400 10900(reheat) (13 200) (15 100)

rpm 8400 8400

TET (C°) 885 920(F°) 1625 1690

pressure ratio: 5.7 6.15

compressor stages: 9 9max. diameter (mm/in):1020 / 40.2

101 9K

Dassault Mirage IV